1999 Falcon 900C

KEY FEATURES
TOTAL TIME: 3,922 LANDINGS: 2,303

ENGINES: GARRETT TFE-731-5BR-1C ENROLLED ON MSP GOLD

LEFT CENTER RIGHT
TOTAL TIME SINCE NEW: 3,841 3,912 3,841
CYCLES SINCE NEW: 2,273 2,297 2,273
LAST MPI (HRS/CYCLES): 2,199/1,189 2,537/1,347 2,199/1,189
NEXT CZI: 5,000 5,000 5,000
SERIAL NUMBER: P-101355 P-101356 P-101353

APU: GARRETT GTCP 36-150F

SERIAL NUMBER: P-347 ENROLLED ON MSP GOLD

TSN: 1,986

WEIGHT:
MAX RAMP WEIGHT: 46,700 LBS. MAX TAKE-OFF WEIGHT: 46,500 LBS.
MAX LANDING WEIGHT: 42,000 LBS. MAX ZERO FUEL WEIGHT: 30,870 LBS.
EMPTY WEIGHT: 25,174 LBS. MIN FLIGHT WEIGHT: 20,700 LBS.

CAPABILITIES:
WAAS/LPV TCAS 7.1
ADS-B OUT V2 PRNAV
FMS 6.1 EGPWS W/ RAAS
GOGO BIZ AVANCE L3 DU-875

AVIONICS
AIR DATA COMPUTER: DUAL HONEYWELL DU 875 AIR DATA COMPUTERS
AUTOMATIC DIRECTION FINDER: DUAL COLLINS ADF-462
AUTOPILOT / FLIGHT DIRECTOR: DUAL HONEYWELL FZ-800 AUTOPILOT COMPUTERS
COCKPIT VOICE RECORDER: HONEYWELL SOLID STATE COCKPIT VOICE RECORDER (120 MINUTE) COMMUNICATIONS: TRIPLE COLLINS VHF-422C TRANSCEIVERS WITH 8.33 SPACING AND FM IMMUNITY
DISTANCE MEASURING EQUIPMENT: DUAL COLLINS DME-442
EFIS: HONEYWELL PRIMUS FIVE TUBE EFIS
EMERGENCY LOCATOR TRANSMITTER: ADT 406 MHZ ELT
ENHANCED GROUND PROXIMITY WARNING SYSTEM: HONEYWELL MARK V EGPWS
FLIGHT DATA RECORDER: HONEYWELL SOLID STATE FLIGHT DATA RECORDER
FLIGHT MANAGEMENT SYSTEM: HONEYWELL FMZ-2000 FMS WITH TRIPLE FMS CDU-810 DISPLAYS
GLOBAL POSITIONING SYSTEM: DUAL HONEYWELL GNSSU GPS RECEIVERS
HIGH FREQUENCY COMMUNICATION: DUAL COLLINS HF-9034 HF RADIOS
INERTIAL REFERENCE SYSTEM: TRIPLE HONEYWELL INERTIAL REFERENCE SYSTEMS
NAVIGATION: DUAL COLLINS VIR-432 NAVIGATION RECEIVERS
RADAR: HONEYWELL PRIMUS 880 WEATHER RADAR WITH DUAL CONTROLLERS
RADIO ALTIMETER: SINGLE HONEYWELL RT-300 RADIO ALTIMETER
SELCAL: 2-CHANNEL CSD-714 SELCAL DECODER
TRAFFIC COLLISION AVOIDANCE SYSTEM: COLLINS TCAS II WITH CHANGE 7.1
TRANSPONDER: DUAL COLLINS TDR-94D WITH ADS-B OUT VERSION 2
HONEYWELL N1 DEEC’S
DUAL DAVTRON CLOCKS

INTERIOR DESCRIPTION
(REFURBISHED 2018 WESTAR & 2020 BY STANDARD AERO)

BEAUTIFUL TWELVE-PASSENGER INTERIOR WITH A FORWARD FOUR-PLACE LEATHER CLUB-SEATING AREA WITH TWO FOLD-OUT SIDE LEDGE TABLES. THE MID-CABIN IS EQUIPPED WITH A LEFT SIDE LEATHER FOUR-PLACE CONFERENCE GROUP, OPPOSITE A MID-CABIN CREDENZA. A MID-CABIN BULKHEAD SEPARATES THE CONFERENCE GROUP FROM THE AFT CABIN, WHICH FEATURES A LEFT THREE PLACE UPHOLSTERY DIVAN OPPOSITE A SINGLE LEATHER FORWARD-FACING CLUB SEAT. A WELL-EQUIPPED GALLEY, FORWARD CREW LAVATORY, EXECUTIVE AFT LAVATORY, IN-FLIGHT ACCESSIBLE BAGGAGE BAY, AND JUMPSEAT COMPLETE THIS INTERIOR.

INSPECTIONS
INSPECTION LAST COMPLETED NEXT DUE
1C INSPECTION 12/27/2018 @ 3,415 HRS. OCTOBER 2024
2C INSPECTION 02/08/2012 @ 1,827 HRS. OCTOBER 2024
3C INSPECTION 12/27/2018 @ 3,415 HRS.

ENG. #1 –
1000/1400 HR. INSP. 12/27/2018 @ 3,334 HRS. 4,734 HRS.

ENG. #2 –
1000/1400 HR. INSP. 12/15/2014 @ 2,538 HRS. 3,938 HRS.

ENG. #3 –
1000/1400 HR. INSP. 12/27/2018 @ 3,334 HRS. 4,734 HRS.

ENG. #1 –
1200/1650 HR. INSP. 11/08/2013 @ 2,199 HRS. 3,849 HRS.

ENG. #2 –
1200/1650 HR. INSP. 12/18/2014 @ 2,538 HRS. 4,188 HRS.

ENG. #3 –
1200/1650 HR. INSP. 11/08/2013 @ 2,199 HRS. 3,849 HRS.

ENG. #1 – MPI INSP. 11/08/2013 @ 2,199 HRS. 4,780 HRS.
ENG. #2 – MPI INSP. 12/18/2014 @ 2,538 HRS. 5,010 HRS.
ENG. #3 – MPI INSP. 11/08/2013 @ 2,199 HRS. 4,780 HRS.

MAIN LANDING GEAR OH 12/27/2018 @ 1824 CYCLES 1/27/2024 / 6,977
CYCLES